Algorithm of Relative Lambert Transfer Based on Relative Orbital Elements
Author:
Affiliation:
1. Beihang University, 100191 Beijing, People’s Republic of China
2. China Academy of Engineering Physics, 621999 Mianyang, People’s Republic of China
3. China Academy of Space Technology, 100094 Beijing, People’s Republic of China
Funder
National Natural Science Foundation of China
Natural Science Foundation of Beijing Municipality
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.G003348
Reference18 articles.
1. Spaceborne Autonomous Formation-Flying Experiment on the PRISMA Mission
2. Flight Demonstration of Autonomous Noncooperative Rendezvous in Low Earth Orbit
3. New State Transition Matrices for Spacecraft Relative Motion in Perturbed Orbits
4. Two-Point Boundary Value Problem Solutions to Spacecraft Formation Flying
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